View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61939U 26145.55562634 +.00000000 +00000-0 +12535-2 0 00003
2 61939 53.1574 352.1178 0001450 88.8452 271.2732 15.69757648 09
| Epoch (UTC): | 25 May 2026 13:20:06 |
| Eccentricity: | 0.0001450 |
| inclination: | 53.1574° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 352.1178° |
| argument of perigee: | 88.8452° |
| revolutions per day: | 15.69757648 |
| mean anomaly at epoch: | 271.2732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|